Accession Number:
ADA070192
Title:
A Force and Moment Test of a 1/24-Scale F-111 Model at Mach Numbers from 0.7 to 1.3.
Descriptive Note:
Final rept.,
Corporate Author:
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFS TN
Personal Author(s):
Report Date:
1979-03-02
Pagination or Media Count:
16.0
Abstract:
A test program was conducted in the Propulsion Wind Tunnel 16T to determine forces and moments on a 124-scale F-111 model. Data were obtained at Mach numbers from 0.7 to 1.3 at total pressures of 1200 and 2000 psfa. Model angle of attack was varied from -2 to 20 deg at 0-deg sideslip. Sideslip angles were varied from -10 to 10 deg at 10- and 15-deg angles of attack. Author
Descriptors:
Subject Categories:
- Aerodynamics
- Attack and Fighter Aircraft